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Triaxial Woven Fabric Directional Strength Predictor

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See what it looks like

Equal yarn counts in all three directions give true in-plane isotropy. Unbalance them and the fabric has a weak axis again — just a less obvious one.

Construction Yarn sets
N
yarns/cm
yarns/cm
g/m²
Load Case Design
°
×

Strength at Load Direction

— kN/m

All three yarn sets resolved onto the load axis

Directional Response

Strength Along Axial
— kN/m
Strength at 90°
— kN/m
Isotropy Ratio
— ×
Allowable Load
— kN/m
Specific Strength
— kN·m/kg

A resolved-yarn model gives the upper bound: it assumes every yarn reaches its full strength together, which real fabrics do not because the sets are not equally crimped and do not fail simultaneously. Use it to compare constructions and locate the weak direction, then test the laminate.

Using this calculator

About the Triaxial Woven Fabric Directional Strength Predictor

The formula

This is the expression the tool evaluates. Every term is named underneath, with the unit it must be supplied in.

Strength at Load Direction
strengthAtAngle = f( yarnStrength, axialYarnsPerCm, biasYarnsPerCm, fabricGsm, testAngle, safetyFactor )

Each input feeds the expression evaluated in the browser; the symbol table below names every term and its unit.

Symbols used above
SymbolStands forUnit
yarnStrengthStrength per YarnN
axialYarnsPerCmAxial Yarns (0°)yarns/cm
biasYarnsPerCmBias Yarns (each ±60°)yarns/cm
fabricGsmFabric Areal Weightg/m²
testAngleLoad Direction from Axial°
safetyFactorSafety Factor×
strengthAtAngleStrength at Load DirectionkN/m
strengthAtAxialStrength Along AxialkN/m
strengthAtTransverseStrength at 90°kN/m
isotropyRatioIsotropy Ratio×
allowableLoadAllowable LoadkN/m
specificStrengthSpecific StrengthkN·m/kg

How the result is derived

Step by step, from the values you type to the figure on screen.

  1. The 6 inputs are read from the form on every keystroke: Strength per Yarn, Axial Yarns (0°), Bias Yarns (each ±60°), Fabric Areal Weight, Load Direction from Axial and Safety Factor.
  2. Each value is checked against the accepted range in the input table below. A value outside its range stops the calculation rather than producing a misleading figure — the results blank out and a message appears.
  3. The validated values are substituted into the expression above, which resolves Strength at Load Direction together with every supporting figure in one pass — no value is carried over from a previous entry.
  4. The supporting outputs — Strength Along Axial, Strength at 90°, Isotropy Ratio, Allowable Load and Specific Strength — come from the same pass, so they always describe the same case as the headline figure.
  5. Results are rounded for display only. The full-precision value is used throughout the chain, so reading a rounded intermediate figure back into the tool by hand can shift the last digit.

What each input means

Where to read each value on the floor, the unit it must be in, and the range the tool accepts.

InputUnitAccepted rangeDefaultWhat it means
Strength per YarnN1 to 10000 N450
Axial Yarns (0°)yarns/cm0.1 to 50 yarns/cm4
Bias Yarns (each ±60°)yarns/cm0.1 to 50 yarns/cm3
Fabric Areal Weightg/m²20 to 3000 g/m²320
Load Direction from Axial°0 to 90 °30
Safety Factor×1 to 10 ×3

What the tool returns

The headline figure and every supporting value it is built from.

OutputUnitWhat it tells you
Strength at Load Direction (headline result)kN/mAll three yarn sets resolved onto the load axis
Strength Along AxialkN/m
Strength at 90°kN/m
Isotropy Ratio×
Allowable LoadkN/m
Specific StrengthkN·m/kg

Worked example

Given

Strength per Yarn
450 N
Axial Yarns (0°)
4 yarns/cm
Bias Yarns (each ±60°)
3 yarns/cm
Fabric Areal Weight
320 g/m²
Load Direction from Axial
30 °
Safety Factor
3 ×

The tool loads with this case already solved — the Strength at Load Direction shown above is its answer. Change one value and the difference from this baseline is the sensitivity of the result to that variable.

How to use it

  1. Work through the input groups in order — Construction and Load Case. The defaults are a realistic case, so you can change one value at a time and watch what moves.
  2. There is no calculate button. Every figure recalculates as you type or drag, which is what makes this usable for a what-if sweep rather than a single answer.
  3. Read Strength at Load Direction in the dark results panel — that is the headline figure, expressed in kN/m.
  4. Check the supporting rows underneath (Strength Along Axial, Strength at 90°, Isotropy Ratio, Allowable Load and Specific Strength) before acting on the headline — they are where an implausible input usually shows itself first.
  5. Reset to defaults returns every field to the reference case, which is the quickest way to check whether a surprising result came from the tool or from an input you had changed earlier.

Where this is used

  • Process planning — establishing Strength at Load Direction before a trial is booked, so machine time and material in Composites, Aerospace & Automotive Textiles are committed against a calculated figure rather than an estimate.
  • Costing and quotation — Strength at Load Direction is an input to the cost sheet, and quoting from a worked number rather than a remembered one is what keeps a margin intact.
  • Troubleshooting — when the floor result drifts from plan, entering the measured values (starting with Strength per Yarn) shows how much of the gap in Strength at Load Direction each variable explains.
  • Teaching and study — the accepted ranges bracket normal Composites, Aerospace & Automotive Textiles practice, so moving one variable at a time shows the shape of the relationship rather than a single answer.

Assumptions and limits

  • A resolved-yarn model gives the upper bound: it assumes every yarn reaches its full strength together, which real fabrics do not because the sets are not equally crimped and do not fail simultaneously. Use it to compare constructions and locate the weak direction, then test the laminate.
  • Every input is bounded to the range normal practice occupies (Strength per Yarn 1 to 10000 N, Axial Yarns (0°) 0.1 to 50 yarns/cm and Bias Yarns (each ±60°) 0.1 to 50 yarns/cm, and so on for the rest). Those bounds are guard rails against typing errors, not a claim that the formula fails one unit outside them.
  • The calculation is deterministic: the same inputs always give the same result. It carries no allowance for machine condition, operator skill, ambient conditions or lot-to-lot material variation unless an input above explicitly represents one.
  • Nothing is sent anywhere. The maths runs in your browser, so the numbers you type never leave the page.

Questions people ask

What do I need to know before using the Triaxial Woven Fabric Directional Strength Predictor?

Have these to hand: Strength per Yarn, Axial Yarns (0°), Bias Yarns (each ±60°), Fabric Areal Weight, Load Direction from Axial and Safety Factor. With those entered, the tool returns Strength at Load Direction immediately.

What exactly is Strength at Load Direction?

All three yarn sets resolved onto the load axis. It is reported in kN/m. It is derived from Strength per Yarn, Axial Yarns (0°), Bias Yarns (each ±60°), Fabric Areal Weight, Load Direction from Axial and Safety Factor, and is the figure the rest of the Composites, Aerospace & Automotive Textiles calculation is built around.

Which units does this calculator expect?

Enter Strength per Yarn in N, Axial Yarns (0°) in yarns/cm, Bias Yarns (each ±60°) in yarns/cm, Fabric Areal Weight in g/m², Load Direction from Axial in ° and Safety Factor in ×. Mixing unit systems is the most common cause of a result that looks an order of magnitude wrong — convert before typing, not after reading.

What are the other figures under the main result?

They are the intermediate quantities the calculation passes through: Strength Along Axial, Strength at 90°, Isotropy Ratio, Allowable Load and Specific Strength. They are shown because a headline number nobody can trace is a number nobody trusts — checking them against your own expectation is the fastest way to confirm the inputs were read as you intended.

Can I rely on this for a production decision?

A resolved-yarn model gives the upper bound: it assumes every yarn reaches its full strength together, which real fabrics do not because the sets are not equally crimped and do not fail simultaneously. Use it to compare constructions and locate the weak direction, then test the laminate. Treat the output as an engineering estimate that narrows the trial window, not as a substitute for the trial.

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